NEPP Program Task 19-294 Government Working Group Update N - - PowerPoint PPT Presentation

NASA Electronic Parts and Packaging (NEPP) Program

2019 Electronics Technology Workshop

NEPP Program Task 19-294

Government Working Group Update

N

Prepared by: MSFC ES43/Jeff Martin MSFC ES43-JSEG/Kathy Laird June 2019

2

AGENDA

I. Acronyms

• II. Purpose, Objective, & Scope
• III. Accomplishments
• IV. Current Topics

3

Acronyms

AFC Army Futures Command 3D-CT Three Dimensional Computed Tomography 80Au-20Sn 80% Gold 20% Tin AvMC Aviation and Missile Center CE-11 SAE Component Parts Committee CE-12 SAE Solid State Devices Committee CCDC Combat Capabilities Development Command DLA Defense Logistics Agency EP Engineering Practice GSFC Goddard Space Flight Center GWG Government Working Group JEDEC Joint Electronics Device Council JSEG Jacobs Space Exploration Group MDA Missile Defense Agency MIL-PRF Military Performance Specification MIL-STD Military Standard MSFC Marshall Space Flight Center NEPAG NASA Electronic Parts Assurance Group NEPP NASA Electronics Parts and Packaging NRO National Reconnaissance Office NSWC Naval Surface Warfare Center R&R Read & Record QA Qualifying Activity QCI Quality Conformance Inspection QML Qualified Manufacturers Listing SAE Society of Automotive Engineers SMC Space and Missile Center SMD Surface Mounted Device or Standard Microcircuit Drawing SSTC Solid State Technical Committee TM Test Method

Purpose, Objective, Scope, Meetings

GWG was established in January 2017

• Purpose: To discuss in detail government topics from NEPAG

which require additional in-depth technical solutions

• Objective: To establish a one-government stance applicable to

both terrestrial and space programs

• Scope: Attendees represent 7 government agencies and DLA
• Air Force – SMC/The Aerospace Corporation
• Air Force – Wright-Patterson
• Army – AFC CCDC AvMC
• MDA
• NASA Centers
• Navy – NSWC Crane Division
• NRO/The Aerospace Corporation
• Meetings: Held 64 meetings to date

4

• In the 2017/2018 timeframe, GWG developed a unified stance

disapproving two JEDEC Task Group 15-02 X-Ray Seal Voids proposals to change MIL-STD-883 TM2012 lid seal void requirements.

• Initial Proposal: Increase voiding criteria from 75% to 95%

 A GWG consensus objection letter signed by NASA, US Air Force (SMC/AFMC), Navy, and Army representatives was sent to DLA

• Second Proposal: Inclusion of fillet in the intended seal

width

 Two GWG opposition presentations were given by Kathy Laird/NASA-JSEG and Matt Dorcon/NSWC Crane at the JEDEC JC13 Task Group 15-02 X-Ray Seal Voids Meeting in January 2018.

5

Accomplishments

• 1. Radiography Inspection Criteria

• MIL-STD-883K Change 2 TM2012.10 Lid Seal Voids Requirements
• From paragraph 3.10.2.2 Unacceptable construction:
• Any device wherein the integral lid seal is not continuous or is reduced from

its designed sealing width by more than 75 percent.

• Width reduction to less than 75% may be the result of either a single void or

a combination of voids in the same width area (see figure 2012-7).

• Fillets are not included in the designed (intended) sealing width.

6

Accomplishments

• MIL-STD-750 TM2076 Lid Seal Voids Requirements – Includes Fillet
• 1.1.1 Designed sealing width. The metalized area where the package lid overlaps

the package base (see figure 2076–7).

• 1.1.2 Seal fillet. Exuded seal material, usually concave in shape, which extends

from the edge of the package lid to the point of tangency of the package base (see figure 2076–7).

• 3.8.2.3.2 Defective seal (see figure 2076–2). Any device wherein the lid seal

(including the seal fillet when present) is not continuous or is reduced from its designed sealing width by more than 75 percent. The designed sealing width may be reduced by multiple voids (not to include pin hole voids).

NOTE: Expulsion resulting from the final sealing operation is not considered extraneous material as long as it can be established that it is continuous, uniform, and attached to the parent material and does not exhibit a ball, splash, or tear-drop configuration.

7

Accomplishments

• Justification Not to Allow Inclusion of Fillet in Intended Lid Seal

Width

• DLA Land and Maritime has no history of why fillet was included in the seal width for MIL-

STD-750 product (requirement inserted in TM2076 in 1/3/2012)

• M750 has significantly tighter leak rates than M883 and some believe the fillet inclusion was a

compromise since tighter leak rates and this change were made in the same timeframe.

• The fillet is not a design feature of the seal process.
• Fillet width is not a controlled process.
• Fillet forms when solder flows out from under the lid during the sealing process, and tapering
• f the fillet results in a non-uniform seal width (see figures on Slide 8).
• Solder pullback severity can negate the seal effectiveness of the fillet.
• Microcrack(s) not distinguished in x-rays may compromise seal integrity as they can

propagate to a void area when part is placed on board or during box level and system level testing.

8

Accomplishments

• Example 1: Excessive Voiding Underneath Lid
• Voids may reduce sealing width underneath the lid by more than 75% and

also contact the fillet.

• Microcrack(s), not distinguished in x-ray, may compromise seal integrity as they can

propagate to a void area.

• The current lid seal requirements would fail this device, yet pass if the fillet

is included in the intended seal width.

9

This part w as a randomly selected sample and had this void issue. Because this part w as randomly selected, it is highly probable that there are other parts w ith similar issues.

Accomplishments

Source: NASA MSFC Part and Images

• Example 1: Excessive Voiding Underneath Lid (continued)
• The current lid seal requirements would fail this device, yet it would pass if

the fillet is included in the intended seal width.

10

Darkened areas in the designed seal w idth are voids and the fillet w idth tapers (blue arrow ).

Accomplishments

Source: NASA MSFC Part and Images

• Example 2: Excessive Voiding Underneath Lid
• Voids reduce sealing width underneath the lid by more than 75% and

pinholes exist in fillet area next to the lid. Note that the pinholes are not clearly detected in the 2D x-ray image (yellow box) due to the thick, x-ray dense solder of the fillet.

11

2D Image 3D-CT Image

Accomplishments

Source: NASA GSFC Part and MSFC Images

• Example 2: Excessive Voiding Underneath Lid (continued)
• Another 3D-CT image of the device shown on Slide 9. This part would fail

the current criteria, but would pass if the fillet was included in the design

• width. Note the pinholes in the fillet next to the edge of the lid, which

provides a potential leak path.

12

Accomplishments

Source: NASA GSFC Part and MSFC Images

• After the GWG presentations, it was agreed by the JEDEC task group in

January 2018 that the inclusion of the fillet as part of the intended seal width would not be added to MIL-STD-883 TM2012 due to the fact that:

• The formation of the fillet is not a design feature of the seal process. Fillets

form when solder flows out from under the lid during the seal process.

• In most if not all cases, the fillet width by itself would meet the 25%

required seal width.

• The GWG also recommended the fillet allowance stated in MIL-STD-750

TM2076 be removed. This allowance will be removed in the next draft.

• Even though TM1071 leak rate limits are tighter than those given in MIL-STD-

883 TM1014 (with the exception of space level hybrid microcircuits), these tests are performed on pristine product, which does not take into consideration mechanical shock/vibration/thermal stress induced during handling, installation, board/box/system level testing, and end use.

• GWG asked DLA and JEDEC for technical justification of why the fillet was

added in the 1/2012 release. They could not find any technical justification.

13

Accomplishments

• In the 2018/2019 timeframe, a manufacturer requested DLA
• ptimization of TM2012 for their 80Au-20Sn seam sealed packages.

The proposal was to include the fillet as part of the intended seal

• width. This proposal was withdrawn by the mfg.
• GWG demonstrated that this optimization would allow instances of

100% voiding in the seal width area due to the solder fillet meeting the 25% requirement.

 GWG presented the consensus objection letter signed by NASA, US Air Force (SMC/AFMC), Navy, and Army representatives that was sent to DLA for review which opposed 95% voiding.

• GWG contacted a SME at Sandia National Laboratories who has several

studies regarding AU/SN solder seal wetting issues. He advised not to relax the specification. His basis was it is not part of the seal frame joint and it is not load bearing due to the fact it is not wetted to the lid. Additionally, the AWS only recognizes the wetted bond area and has tighter criteria, 70%.

14

Accomplishments

Accomplishments

• 2. Military Document Draft Reviews
• GWG supported the technical review of 6 draft documents and

representatives compiled comments. Comments are submitted to DLA

• r SAE for consideration in the next revision or release.
• MIL-PRF-123 Rev E 2nd Draft “Capacitors, Fixed, Ceramic Dielectric,

(Temperature Stable and General Purpose), High Reliability (Space)”

• MIL-PRF-28750 Rev K Draft “Relays, Solid State, General Specification for”
• MIL-PRF-38534 Rev L Draft “Hybrid Microcircuits, General Specification

for”

• MIL-STD-1580 Rev C Draft Compilation of Comments “Destructive

Physical Analysis for Electronic, Electromagnetic and Electromechanical Parts”

• Members attended Coordination Meeting to adjudicate 218 comments
• SAE AS6294/3 and /4 Requirements for Plastic Encapsulated Microcircuits

Discrete Semiconductors in Space and Military/Avionics Applications

15

Current Topics

Work in Progress

• JEDEC Task Group proposal to change MIL-STD-883 TM2012

X-ray lid seal failure criterion.

16

• Would remove “B + C”

requirement and replace with seal length calculation along perpendicular line drawn from edge of package to cavity

• Would allow fillets to be part of

intended seal width

• GWG does not support this change

From MIL-STD-883K w/Change 1 TM2012.9

(continued on next page)

Current Topics

Work in Progress (cont.)

• JEDEC Task Group proposal to change MIL-STD-883 TM2012

X-ray lid seal failure criterion (cont.)

• These microcircuits would pass the proposed criteria

17

A B

X-ray Image of Voids

Source: A. NASA MSFC JN11-009 SN0079, B. NASA MSFC JN11-009 SN0167

Current Topics

Work in Progress (cont.)

• Polymer Tantalum Capacitor MIL-Spec Development

Working Group Activity Discussions

18

Working Group Focus:

• 1. Develop MIL spec for polymer tantalum capacitors for a diverse range of

applications (e.g., terrestrial airborne space, etc.). Two product levels shall be developed:  M Level for standard product  T Level for hi-rel (e.g., space)

• 2. Develop a series of slash sheets to cover specific product families/constructions

Possibilities include:  Standard single anode  Multi anode  Molded case vs. conformal coat  Hermetic leaded and hermetic surface mount capacitors most likely will not be included with this working group effort

Current Topics

Work in Progress (cont.)

• Data Retention Requirements
• Current data retention requirements are not the same for all commodities:

19

MIL-PRF-38534: 3 years all Classes except Class K; Class K: 7 years MIL-PRF-38535: 5 years (records pertaining to screening and quality conformance) MIL-PRF-19500: 10 years MIL-STD-790: The records pertaining to production processes, incoming, and in- process inspections should be retained for a minimum of 3 years (7 years for space level) and those pertaining to performance verification retained for a minimum of 5 years (7 years for space level) after performance of the inspections. Records pertaining to alternate methods (with qualifying activity approval), conformance testing shall be retained for 5 years (7 years for space level) after the process or materials affected have been removed from the qualified flow.

• GWG requested DLA to perform an EP Study. We provided proposed

wording and survey questions for manufacturers input.

Current Topics

Work in Progress (cont.)

• Data Retention Requirements (cont.)

20 Record retention. The manufacturer of QML devices (all class levels) shall retain all design, manufacturing, testing and quality records for each lot for a period of 15 years after delivery of product. The records shall include as a minimum: a. Design b. Manufacturing c. Travelers d. Inspection e. Test results f. Screening results g. Qualification plans and results h. Quality conformance test results i. Rework j. Failure analysis and corrective actions k. TRB decisions l. Training m. Customer returns The records shall be retained in the form in which they were originally defined but electronic media is preferred and a copy shall be provided to the qualifying and/or procuring activity as requested.

• The proposed requirement wording consisted of the following:

Current Topics

Work in Progress (cont.)

• Data Retention Requirements (cont.)

21

• 1. What is the standard amount of time manufacturers retain data

for military products? For commercial products?

• 2. Is a proposed 15 year retention time acceptable?
• 3. What concerns do manufacturers have with retaining records

electronically?

• 4. Can all lot data be retained, including travelers, incoming

inspection, R&R, screening, QCI, etc. If the answer is no, what data can be retained?

• 5. What financial hardship, if any, would this endeavor impose?
• 6. For users of military devices, are there any additional types of

data that you would like to see retained?

• The EP Study survey questions posed were as follows:

• Data Retention Requirements (cont.)
• DLA conducted 2 EP Studies to ensure adequate distribution to all
• technologies. Regarding the survey question as to whether a 15
• yr. retention time was acceptable:

 1st Study (MIL-PRF-19500,-38534,-38535): 14 responses  5 Yes, 5 No, 3 agreeable to 10 yrs., 1 concerned with cost  2nd Study (MIL-STD-790): 12 responses  7 Yes, 5 No (feedback indicated current retention times varied from 5 -25 yrs.

for military product and 0 -10 yrs. for commercial product)

• DLA decided against an all encompassing specification change
• GWG decided to pursue a compromised 10 yr. retention time in

the next revisions of MIL-PRF-38534, -38535 and MIL-STD-790

22

Current Topics

Work in Progress (cont.)

• MIL-STD-750 & -883 TM1018 Internal Gas Analysis
• Concerns:

 IGA/RGA has been at the center of controversy in regards to correlation between test labs and “RGA Roulette”  GWG technically discussed a problem advisory where two associated test labs performed small volume testing without DLA lab suitability

• Response:

 GWG is collaborating with a third party to develop a verification process to confirm test equipment capability

23

Current Topics

Work in Progress (cont.)

• Miscellaneous
• Additional Topics Addressed in Meetings:

 EP Studies  RHA qualification concerns in specification documents  Data sensitive issues:

• Manufacturers concerns and process improvements
• Findings from audits/pre-cap inspections
• Future Topics:

 Review test methods of MIL-STD-202  Standardization of connector specifications  Glass transition temperature (Tg) concerns for plastics

24

Current Topics

Work in Progress (cont.)

Questions?

Contact Information:

• Kathy.R.Laird@nasa.gov
• Jeffrey.H.Sokol@aero.org